FR1556422A - - Google Patents
Info
- Publication number
- FR1556422A FR1556422A FR1556422DA FR1556422A FR 1556422 A FR1556422 A FR 1556422A FR 1556422D A FR1556422D A FR 1556422DA FR 1556422 A FR1556422 A FR 1556422A
- Authority
- FR
- France
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB610967A GB1150123A (en) | 1967-02-08 | 1967-02-08 | Improvements in or relating to the Construction of Rotor Blades for Rotary Wing Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1556422A true FR1556422A (enrdf_load_stackoverflow) | 1969-02-07 |
Family
ID=9808553
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1556422D Expired FR1556422A (enrdf_load_stackoverflow) | 1967-02-08 | 1968-01-05 |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1556422A (enrdf_load_stackoverflow) |
GB (1) | GB1150123A (enrdf_load_stackoverflow) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3952601A (en) * | 1974-12-18 | 1976-04-27 | United Technologies Corporation | Helicopter rotor blade balancing method |
US4275994A (en) * | 1978-04-03 | 1981-06-30 | Textron, Inc. | Roll formed blade structure |
CN112407251A (zh) * | 2020-10-28 | 2021-02-26 | 成都飞机工业(集团)有限责任公司 | 一种火箭弹射无人机配重重心调整方法 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7083383B2 (en) * | 2004-04-26 | 2006-08-01 | The Boeing Company | Segmented rotor blade trim tab |
CN106005397A (zh) * | 2016-07-14 | 2016-10-12 | 上海未来伙伴机器人有限公司 | 多旋翼机桨、多旋翼机以及改善桨叶静不平衡的方法 |
-
1967
- 1967-02-08 GB GB610967A patent/GB1150123A/en not_active Expired
-
1968
- 1968-01-05 FR FR1556422D patent/FR1556422A/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3952601A (en) * | 1974-12-18 | 1976-04-27 | United Technologies Corporation | Helicopter rotor blade balancing method |
US4275994A (en) * | 1978-04-03 | 1981-06-30 | Textron, Inc. | Roll formed blade structure |
CN112407251A (zh) * | 2020-10-28 | 2021-02-26 | 成都飞机工业(集团)有限责任公司 | 一种火箭弹射无人机配重重心调整方法 |
CN112407251B (zh) * | 2020-10-28 | 2023-01-10 | 成都飞机工业(集团)有限责任公司 | 一种火箭弹射无人机配重重心调整方法 |
Also Published As
Publication number | Publication date |
---|---|
GB1150123A (en) | 1969-04-30 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |